EP 3661846 B1 20230614 - HYBRID AERIAL VEHICLE
Title (en)
HYBRID AERIAL VEHICLE
Title (de)
HYBRIDES LUFTFAHRZEUG
Title (fr)
VÉHICULE AÉRIEN HYBRIDE
Publication
Application
Priority
- US 201762540075 P 20170802
- IL 2018050860 W 20180802
Abstract (en)
[origin: WO2019026079A1] A hybrid aerial vehicle (HAV) comprising: a fuselage of the HAV; a first mechanism within the fuselage for accepting a plurality of wings of the HAV, the first mechanism allowing coordinated contraction of the plurality of wings essentially into the fuselage such that tips of the wings are position in proximity of the fuselage and coordinated extension of the wings such that tips of each wing are positioned away from the fuselage; a first wing extending from the port side of the fuselage and connected to the first mechanism; a second wing extending from the starboard side of the fuselage and connected to the first mechanism; a second mechanism placed within the fuselage in proximity to its front end, the second mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain; a first set of propellers affixed at the port side of the fuselage to the second mechanism; a second set of propellers affixed at the starboard side of the fuselage to the second mechanism; a third mechanism placed within the fuselage in proximity to its rear end, the third mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain, and further placing the propellers affixed thereto to be at a vertical displacement with respect to the propellers affixed to the second mechanism; a third set of propellers affixed at the port side of the fuselage to the third mechanism; and a fourth set of propellers affixed at the starboard side of the fuselage to the third mechanism.
IPC 8 full level
B64C 29/00 (2006.01); B64C 3/40 (2006.01); B64C 3/56 (2006.01); B64C 25/52 (2006.01); B64C 27/28 (2006.01); B64C 27/52 (2006.01); B64F 1/22 (2006.01); B64F 1/24 (2006.01); B64F 1/32 (2006.01); B64C 25/32 (2006.01); B64D 27/02 (2006.01)
CPC (source: EP IL US)
B64C 3/40 (2013.01 - EP IL); B64C 13/34 (2013.01 - IL US); B64C 13/50 (2013.01 - IL US); B64C 25/52 (2013.01 - EP IL); B64C 29/0033 (2013.01 - EP IL US); B64D 27/02 (2013.01 - EP IL); B64D 27/026 (2024.01 - EP IL); B64F 1/22 (2013.01 - EP IL); B64F 1/24 (2013.01 - EP IL); B64F 1/32 (2013.01 - EP IL); B64U 10/14 (2023.01 - EP IL US); B64U 30/12 (2023.01 - EP IL US); B64U 30/26 (2023.01 - EP IL US); B64U 30/297 (2023.01 - EP IL US); B64U 40/10 (2023.01 - EP IL US); B64U 50/12 (2023.01 - EP IL US); B64U 50/14 (2023.01 - EP IL US); B64U 50/19 (2023.01 - EP IL US); B64U 50/33 (2023.01 - EP IL US); B64U 70/30 (2023.01 - EP IL US); B64C 2025/325 (2013.01 - EP IL); B64U 2101/64 (2023.01 - US); Y02T 50/10 (2013.01 - EP IL); Y02T 50/60 (2013.01 - EP IL)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2019026079 A1 20190207; AU 2018311641 A1 20200220; CN 111295330 A 20200616; EP 3661846 A1 20200610; EP 3661846 A4 20210811; EP 3661846 B1 20230614; EP 3661846 C0 20230614; EP 4039590 A1 20220810; EP 4039590 B1 20230607; EP 4039590 C0 20230607; EP 4043345 A1 20220817; ES 2954742 T3 20231124; ES 2955333 T3 20231130; HR P20230949 T1 20231124; HR P20230950 T1 20231208; IL 272347 A 20200331; IL 302650 A 20230701; US 11584524 B2 20230221; US 2020239137 A1 20200730
DOCDB simple family (application)
IL 2018050860 W 20180802; AU 2018311641 A 20180802; CN 201880050566 A 20180802; EP 18842298 A 20180802; EP 22165553 A 20180802; EP 22166014 A 20180802; ES 18842298 T 20180802; ES 22165553 T 20180802; HR P20230949 T 20180802; HR P20230950 T 20180802; IL 27234720 A 20200129; IL 30265023 A 20230503; US 201816635010 A 20180802